ELECTRON R/B
NORAD 100683
Rocket Body
LEO
2026-207B
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LEO · NORAD 100683
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
193 km
Apogee
492 km
Inclination
36.1°
Period
91.4 min
Mean Motion
15.75718567 rev/day
TLE Epoch
2026-09-11 13:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude343 km
Orbital Velocity27,739 km/h
Velocity7.71 km/s
Orbital Period91 minutes
Orbits / Day15.76
Eccentricity0.0223
Semi-Major Axis6,714 km
Est. Orbital LifetimeMonths to ~1 year
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
2026-09-11
Launch Site
RLLC
Int'l Designator
2026-207B
Object Type
Rocket Body
RCS Size
Unknown
📖 About This Object
ELECTRON R/B is a spent rocket body associated with United States, launched on 2026-09-11 from RLLC. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. It orbits in Low Earth Orbit (LEO) at altitudes between 193 km and 492 km with an inclination of 36.1°. It travels at approximately 27,739 km/h (7.71 km/s), completing one full orbit every 91 minutes — that’s roughly 15.76 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is months to ~1 year. Spent rocket bodies like ELECTRON R/B are among the largest pieces of uncontrolled space debris and are priority targets for collision avoidance manoeuvres and future active debris removal efforts.
🌍 Orbit Context
ELECTRON R/B orbits at an average altitude of 343 km in the lower reaches of Low Earth Orbit, where atmospheric drag is significant and orbital lifetimes are measured in months to a few years. This is the busiest corridor in space — home to crewed spacecraft, rapid-revisit imaging satellites and the densest part of the Starlink constellation. Within ±50 km of ELECTRON R/B’s average altitude, there are currently 1,221 active payloads and 38 tracked debris or rocket body fragments — notable neighbours include STARLINK-1008, STARLINK-1012, STARLINK-1020. This makes it one of the more crowded altitude bands, containing roughly 6.7% of all active satellites. With an inclination of 36.1°, ELECTRON R/B passes over latitudes between 36.1°N and 36.1°S, covering the tropical and temperate zones where most of the world’s population resides. Low-to-mid inclination orbits are efficient to reach from equatorial and mid-latitude launch sites. United States operates approximately 12,945 active satellites in total, of which 1,144 share a similar altitude band with ELECTRON R/B.
🔗 Spent Rocket Body
This is a spent rocket body — the upper stage of a launch vehicle that remains in orbit after delivering its payload. Rocket bodies are a significant contributor to the space debris population. Older stages often retained residual propellant that could later explode, creating debris fields. Modern guidelines require upper stages to either deorbit (controlled re-entry) or passivate (vent residual fuel) to reduce fragmentation risk. The FCC's 5-year deorbit rule and UN debris mitigation guidelines are increasingly enforced to address this growing problem.
❓ Frequently Asked Questions
ELECTRON R/B orbits in Low Earth Orbit (LEO) at altitudes between 193 km (perigee) and 492 km (apogee), with an average altitude of approximately 343 km. It completes one orbit every 91 minutes, travelling at approximately 27,739 km/h (17,236 mph).
ELECTRON R/B (NORAD ID 100683) is a spent rocket body — the upper stage of a launch vehicle attributed to United States. It no longer serves a functional purpose but continues to orbit Earth as tracked debris. Spent upper stages are among the largest uncontrolled objects in orbit and are closely monitored for collision risk.
ELECTRON R/B was launched on 2026-09-11 from RLLC. At its current altitude, the estimated remaining orbital lifetime is: months to ~1 year. View the full satellite launch log.
Yes — Orbital Radar tracks ELECTRON R/B (NORAD ID 100683) using the latest TLE (two-line element set) data from Space-Track and CelesTrak. Open the live tracker to see its current position, altitude, speed and orbital path updated in real time. You can also browse the satellite directory to find other tracked objects.
ELECTRON R/B travels at approximately 27,739 km/h (17,236 mph) — roughly 7.71 km/s. It completes 15.76 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 32 sunrises and sunsets every 24 hours.